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Inventor profile of:

PRATT & WHITNEY CANADA CORP.

City:

Country:

United States

Published Applications:

17

Last publication date:

2015-07-09

Top Assignees for applications by PRATT & WHITNEY CANADA CORP.

The entities that hold a legal rights for patent applications filed by inventor PRATT & WHITNEY CANADA CORP.:

Recent patent applications by PRATT & WHITNEY CANADA CORP.

PRATT & WHITNEY CANADA CORP. from , US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2015-07-09
US20150192069A1
Mechanical engineering

Recuperator for gas turbine engine

 #2 | 2014-12-04
US20140356159A1
Mechanical engineering

Low hub-to-tip ratio fan for a turbofan gas turbine engine

 #3 | 2014-11-20
US20140338346A1
Mechanical engineering

Combustor skin assembly for gas turbine engine

 #4 | 2014-10-02
US20140297155A1
Performing operations; transporting

Aircraft power outtake management

 #5 | 2014-10-02
US20140291987A1
Mechanical engineering

Engine architecture using electric machine

 #6 | 2014-10-02
US20140290265A1
Mechanical engineering

Gas turbine engine with transmission

 #7 | 2014-09-25
US20140286746A1
Mechanical engineering

Compressor shroud reverse bleed holes

 #8 | 2014-09-18
US20140260296A1
Mechanical engineering

Slinger combustor

 #9 | 2014-09-18
US20140260266A1
Mechanical engineering

Combustor for gas turbine engine

 #10 | 2014-09-04
US20140245988A1
Mechanical engineering

Rotary internal combustion engine with pilot subchamber

 #11 | 2014-08-28
US20140241901A1
Mechanical engineering

Impeller

 #12 | 2014-08-28
US20140241899A1
Mechanical engineering

BLADE LEADING EDGE TIP RIB

 #13 | 2014-08-28
US20140241854A1
Mechanical engineering

Active turbine or compressor tip clearance control

 #14 | 2014-08-07
US20140219817A1
Mechanical engineering

High pressure turbine blade cooling hole distribution

 #15 | 2014-08-07
US20140219816A1
Mechanical engineering

High pressure turbine blade cooling hole distribution

 #16 | 2014-06-05
US20140150449A1
Mechanical engineering

Air cooling shaft at bearing interface

 #17 | 2013-10-10
US20130263603A1
Mechanical engineering

Nozzle design to reduce fretting
InventorID:

472576 ⎘